What was found
LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.643", FINAL HOLE DIA: 0.716", MAXIMUM ALLOWABLE DIA: 0.709". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892, PART 1, STEP 1B WINGS-FLIGHT SURFACES EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.